Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 60 ̊
By: Thomas M. Moul ... [et al.].
Contributors: Moul, Thomas M.; Langley Research Center.
Series: NASA technical memorandum -- 4649.
Publisher: National Aeronautics and Space Administration, Langley Research Center; Available from the National Technical Information Service
Published: 1995
Place of publication: Hampton, Va; Springfield, VA
Language: eng
Number of pages: 155
Subjects: Stability of airplanes; Airplanes -- Wings
Other titles: Low speed wind tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 60.̊
Notes: "August 1995."

"Performing organization report number L-17400"--Report documentation page.

Includes bibliographical references (p. 13-14).

Available electronically at the following URL address: http://techreports/larc.nasa.gov/ltrs/ltrs.html.

Performed by Langley Research Center for the National Aeronautics and Space Administration WU 505-68-30-01.